GB1014165A - Improvements in and relating to jet propulsion engine afterburner fuel-flow control systems - Google Patents

Improvements in and relating to jet propulsion engine afterburner fuel-flow control systems

Info

Publication number
GB1014165A
GB1014165A GB36177/62A GB3617762A GB1014165A GB 1014165 A GB1014165 A GB 1014165A GB 36177/62 A GB36177/62 A GB 36177/62A GB 3617762 A GB3617762 A GB 3617762A GB 1014165 A GB1014165 A GB 1014165A
Authority
GB
United Kingdom
Prior art keywords
spring
jet propulsion
propulsion engine
relating
flow control
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB36177/62A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Parker Hannifin Corp
Original Assignee
Parker Hannifin Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Parker Hannifin Corp filed Critical Parker Hannifin Corp
Publication of GB1014165A publication Critical patent/GB1014165A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/228—Dividing fuel between various burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

1,014,165. Valves. PARKER-HANNIFIN CORPORATION. Sept. 24, 1962 [Oct. 11, 1961], No. 36177/62. Heading F2V. [Also in Division F1] A valve unit 53 for the control of fuel flowing to a jet propulsion engine afterburner comprises a member 63 sliding in a bore 61 under the action of spring 65 and spring 82 connected to member 63 by sliding abutment 81 and rod 66 having a head 80 sliding in the abutment 81. On receiving a fluid pressure signal from the afterburner fuel control unit through the line 47 a spring-loaded piston 83 moves to the left and head 86 of rod 85 contacts abutment 81 and relieves valve member 63 of the force of spring 82, thus lowering the opening pressure of the valve.
GB36177/62A 1961-10-11 1962-09-24 Improvements in and relating to jet propulsion engine afterburner fuel-flow control systems Expired GB1014165A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US144330A US3197958A (en) 1961-10-11 1961-10-11 Fuel selector and flow divider valve and control means for jet engines

Publications (1)

Publication Number Publication Date
GB1014165A true GB1014165A (en) 1965-12-22

Family

ID=22508109

Family Applications (1)

Application Number Title Priority Date Filing Date
GB36177/62A Expired GB1014165A (en) 1961-10-11 1962-09-24 Improvements in and relating to jet propulsion engine afterburner fuel-flow control systems

Country Status (4)

Country Link
US (1) US3197958A (en)
BE (1) BE619221A (en)
DE (1) DE1426418A1 (en)
GB (1) GB1014165A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2167808A (en) * 1984-11-30 1986-06-04 Pierburg Gmbh & Co Kg I C engine fuel flow regulating system

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1388004A (en) * 1963-11-27 1965-02-05 Device for starting and controlling the operation of a gas turbine power generator
US3293858A (en) * 1965-02-04 1966-12-27 Chandler Evans Inc Flow division apparatus for fuel supply system
GB1284287A (en) * 1968-10-10 1972-08-02 Snecma A device for programming the ignition stage of the re-heat combustion in a gas turbine power plant
US3793825A (en) * 1972-01-27 1974-02-26 Ford Motor Co Time delay gas turbine starting system with fuel pressure and flame sensing circuitry
GB1423362A (en) * 1972-06-21 1976-02-04 Lucas Industries Ltd Fuel control apparatus for gas turbine engine reheat systems
US3977376A (en) * 1974-11-14 1976-08-31 Cummins Engine Company, Inc. Diesel engine intake air preheater fuel control
US4033116A (en) * 1975-09-23 1977-07-05 Vasily Petrovich Dmitriev Fuel distribution arrangement
US5003771A (en) * 1988-10-13 1991-04-02 United Technologies Corporation Fuel distribution valve for a combustion chamber
CN113202633B (en) * 2021-04-28 2022-06-07 中国航发沈阳发动机研究所 Method for designing oil supply rule of small bypass ratio integrated afterburner

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2937501A (en) * 1955-07-13 1960-05-24 Sud Aviation Combustion devices for ram-jet engines
US2845079A (en) * 1956-02-06 1958-07-29 Pierce Governor Company Inc Fuel flow divider
US2938341A (en) * 1957-01-18 1960-05-31 Lucas Industries Ltd Valves for controlling re-heat fuel on air-craft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2167808A (en) * 1984-11-30 1986-06-04 Pierburg Gmbh & Co Kg I C engine fuel flow regulating system

Also Published As

Publication number Publication date
US3197958A (en) 1965-08-03
BE619221A (en) 1962-12-21
DE1426418A1 (en) 1969-01-23

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